EP 1943145 B1 20090218 - TURBOJET ENGINE FRONT FASTENING DEVICE PROVIDED WITH A STRUT FOR FIXING TO AN AIRCRAFT
Title (en)
TURBOJET ENGINE FRONT FASTENING DEVICE PROVIDED WITH A STRUT FOR FIXING TO AN AIRCRAFT
Title (de)
BEFESTIGUNGSVORRICHTUNG FÜR EINEN TURBOSTRAHLMOTOR MIT EINER STREBE ZUR BEFESTIGUNG AN EINEM FLUGZEUG
Title (fr)
DISPOSITIF D'ATTACHE AVANT D'UN TURBOREACTEUR A UN MÂT DE FIXATION D'UN AERONEF
Publication
Application
Priority
- FR 2006051093 W 20061024
- FR 0553304 A 20051031
Abstract (en)
[origin: FR2892706A1] The device has a top bracket (101) and a lower bracket (102), primary fixing points connecting the bracket (102) to the bracket (102), and secondary fixing points connecting the bracket (102) to an aircraft turbojet engine. A thrust load absorption vector (V) results from a convergence point (C1) of primary vectors passing via the primary fixing points and from a convergence point (C2) of secondary vectors passing via the secondary fixing points. The vector (V) transfers turbojet engine thrust loads to an aircraft fixing strut (3) and extends along a turbojet engine axis (A). The secondary fixing points are constituted by a rudder control bar, a secondary rear control rod and a secondary front control rod. An independent claim is also included for a turbojet engine front fastening device and a turbojet engine assembly.
IPC 8 full level
B64D 27/40 (2024.01)
CPC (source: EP US)
B64D 27/40 (2024.01 - EP US); B64D 27/406 (2024.01 - EP); B64D 27/406 (2024.01 - US)
Designated contracting state (EPC)
AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC NL PL PT RO SE SI SK TR
DOCDB simple family (publication)
FR 2892706 A1 20070504; FR 2892706 B1 20090424; AT E423061 T1 20090315; BR PI0618083 A2 20110816; CA 2625800 A1 20070510; CA 2625800 C 20130611; CN 101300172 A 20081105; DE 602006005263 D1 20090402; EP 1943145 A2 20080716; EP 1943145 B1 20090218; JP 2009513434 A 20090402; JP 5227798 B2 20130703; RU 2008121952 A 20091210; RU 2398715 C2 20100910; US 2009218441 A1 20090903; US 8366038 B2 20130205; WO 2007051938 A2 20070510; WO 2007051938 A3 20070719
DOCDB simple family (application)
FR 0553304 A 20051031; AT 06831287 T 20061024; BR PI0618083 A 20061024; CA 2625800 A 20061024; CN 200680040422 A 20061024; DE 602006005263 T 20061024; EP 06831287 A 20061024; FR 2006051093 W 20061024; JP 2008537157 A 20061024; RU 2008121952 A 20061024; US 8439306 A 20061024